EP0245533B1 - Three dimensional woven fabric connector - Google Patents
Three dimensional woven fabric connector Download PDFInfo
- Publication number
- EP0245533B1 EP0245533B1 EP86106650A EP86106650A EP0245533B1 EP 0245533 B1 EP0245533 B1 EP 0245533B1 EP 86106650 A EP86106650 A EP 86106650A EP 86106650 A EP86106650 A EP 86106650A EP 0245533 B1 EP0245533 B1 EP 0245533B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- section
- sections
- fabric
- interwoven
- intersection
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
- 239000002759 woven fabric Substances 0.000 title claims abstract description 17
- 239000000835 fiber Substances 0.000 claims abstract description 104
- 239000004744 fabric Substances 0.000 claims abstract description 53
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 2
- 239000011152 fibreglass Substances 0.000 claims description 2
- 229910002804 graphite Inorganic materials 0.000 claims description 2
- 239000010439 graphite Substances 0.000 claims description 2
- 239000011800 void material Substances 0.000 claims 1
- 238000009941 weaving Methods 0.000 description 4
- 238000010276 construction Methods 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 229920000271 Kevlar® Polymers 0.000 description 1
- 239000000853 adhesive Substances 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 239000004761 kevlar Substances 0.000 description 1
- 239000011347 resin Substances 0.000 description 1
- 229920005989 resin Polymers 0.000 description 1
Images
Classifications
-
- D—TEXTILES; PAPER
- D03—WEAVING
- D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
- D03D3/00—Woven fabrics characterised by their shape
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/06—Fibrous reinforcements only
- B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
- B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
- B29C70/24—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least three directions forming a three dimensional structure
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
- B29D24/00—Producing articles with hollow walls
- B29D24/002—Producing articles with hollow walls formed with structures, e.g. cores placed between two plates or sheets, e.g. partially filled
- B29D24/004—Producing articles with hollow walls formed with structures, e.g. cores placed between two plates or sheets, e.g. partially filled the structure having vertical or oblique ribs
-
- D—TEXTILES; PAPER
- D03—WEAVING
- D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
- D03D25/00—Woven fabrics not otherwise provided for
- D03D25/005—Three-dimensional woven fabrics
Definitions
- This invention relates to a fabric joint for providing three-dimensional structural support, to a three-dimensional woven connector formed by said joint and to the application of said joint for joining structural aircraft components.
- a type of a fabric joint connector is known from applications in the aircraft industry to join structural components such as spars or ribs to wing skin coverings. Said L-shaped fabric joint connectors are bonded by adhesive to both structural components. Although creating a light-weighted joint, typical strength and efficient load transfer in only a limited number of directions is achieved, while presenting weaknesses in other directions, which, e.g. lead to peeling problems.
- a joint known from US-A 4 395 450 contains a resin impregnated woven fabric connector with intersecting fabric panels which are interwoven with an intermediate laterally extending panel.
- the connector is used for joints of aircraft structural members.
- the fiber orientation is predominately transverse.
- Woven fabric material for high load applications is known from US-A 3 991 249 and US-A 3 090 406 in which intersecting fabric sections use at least one common weft thread.
- the line of intersection between the sections of the fabric material extends perpendicular to the weaving or warp direction.
- DE-C 357 353 and US-A 3 538 957 disclose three-dimensional fabric having lines of intersection between connected sections of the fabric, said lines of intersection extending in weaving or warp direction.
- FIG. 1 shows a prior art arrangement for connecting a spar or rib 4 (such as might be used in construction of an airplane wing) to another structural component 8 (such as the skin or covering of an aircraft wing).
- a pair of fabric connectors 12 and 16 Placed at the joint of the spar 4 and structural component 8 to hold the two together are a pair of fabric connectors 12 and 16 (shown in cross section in FIG. 1). A portion of each fabric connector 12 and 16 is placed flat against and bonded to the structural component 8 while another portion is placed flat against and bonded to the spar 4 as shown.
- This connector arrangement provides fairly good strength and load transfer efficiency between the spar 4 and structural component 8 when the two components are moved as indicated by arrows 20 relative to one another.
- the strength of the connector is very weak when the two components are moved in the direction indicated by arrows 24 and 28 relative to one another. In particular, such movement would give rise to well known fabric connector peel problems.
- the three-dimensional woven fabric connector of the present invention avoids the problems outlined in connection with the FIG. 1 arrangement, and one embodiment of the connector is shown in fragmented, cross-sectional view in FIG. 2.
- This embodiment is shown connecting a spar 34 to a skin covering 38, such as used in the construction of aircraft. It is noted that both the spar 34 and skin covering 38 are shown as being made of a sandwich wall construction.
- the woven fabric connectors of the present invention may be used to connect together a variety of structural components in addition to those shown in the drawings.
- the connector embodiment of FIG. 2 includes a first section of fabric 40 composed of fibers interwoven together in a cross-hatched pattern as will be described in detail later. Also included are second and third sections of fabric 44 and 48 also composed of fibers interwoven together in a cross-hatched fashion. The second and third sections of fabric 44 and 48 are also interwoven with the first section 40 along respective intersections 52 and 56 of the sections. The locus of points at which section 44 intersects section 40 and the locus of points at which section 48 intersects section 40 are spaced apart and generally parallel in the plane of section 40. As will be explained further later on, at least one fiber or fiber bundle of the section of fabric 40 is common with the section of fabric 44, and at least one other fiber or fiber bundle of section 40 is common with section 48.
- portions of both sections 44 and 48 extend upwardly from section 40 and portions also extend downwardly therefrom.
- a portion of section 40 extends outwardly in one direction from section 44, and another portion of section 40 extends outwardly in the opposite direction from section 48, with an intermediate portion of section 40 extending between sections 44 and 48.
- the sections 44 and 48 are shown as intersecting section 40 at right angles, but other angles of intersection could also be used as needed. Additionally, the fabric sections are bendable and thus may be made to conform to variety of shapes to which they might be bonded.
- the spar 34 and skin cover 38 are connected together by placing section 44 flat against the underside of the skin covering 38 and bonding it thereto.
- the two upper portions of sections 44 and 48 extend into the skin covering 38 and are bonded to the interior of the skin section covering.
- the edge of the spar 34 is placed between the two lowermost portions of sections 44 and 48 and is bonded therebetween.
- a spar section 60 is also positioned between the two upper portions of the sections 44 and 48 as shown in FIG. 2.
- FIG. 3 is a cross-sectional view of another embodiment of the woven fabric connector of the present invention. This embodiment also is shown coupling together a spar 64 to a skin covering 68.
- the connector of FIG. 3 includes a first section of woven fabric 72, and second and third sections of woven fabric 76 and 80 which are interwoven with the section 72 to extend downwardly therefrom as shown.
- the sections of fabric 76 and 78 intersect the section of fabric 72 along generally parallel loci of points at which intersections a fiber or bundle of fibers is common with the section 72 and respective sections 76 and 80.
- the connector of FIG. 3 is utilized by placing section 72 flat against the bottom surface of the skin covering 68 and bonding it thereto.
- the spar 64 is positioned between sections 76 and 80 and is bonded to the sections, and to the underside of section 72.
- FIG. 4 shows a cross-sectional view of still another embodiment of the woven fabric connector of the present invention.
- two connectors 84 and 88 are shown interconnecting, at a right angle, the edges of two skin covers 92 and 96.
- Each of the connectors, such as connector 84 includes three sections 100, 104 and 108, all of which extend generally radially outwardly from an intersection 112 of the three sections.
- the three sections are composed of fibers interwoven together, with at least one fiber or bundle of fibers being common to the three sections.
- the connector 88 is similar to the connector 84 except two of the sections are bent to overlie the outside corner of the joint of the two skin coverings 92 and 96, as shown. Two of the sections of connectors 84 and 88 extend into the joint between the skin coverings 92 and 96 generally in planes parallel to one another. The different sections of the two connectors 84 and 88 are bonded to the surfaces of the skin coverings with which they are placed in contact.
- FIG. 5 shows a schematic representation of the weaving of the connector embodiment of FIG. 2.
- the connector incudes lengthwise fibers or fiber bundles 120 which serve as the warp of the woven fabric. Interlaced through the lengthwise fibers 120 or warp are crosswise fibers or fiber bundles 124 which serve as the weft of the fabric.
- the crosswise fibers 124 of section 48 are interwoven about a lengthwise fiber or bundle of fibers 56 which is common and serves as an intersection with section 40.
- the crosswise fibers 124 of the section 44 are interwoven with a lengthwise fiber or bundle of fibers 52 which is also common with the section 40.
- the common fiber or fiber bundle 52 is spaced from and generally parallel with the fiber or fiber bundle 56, as indicated in FIG. 5.
- the crosswise fibers 124 are interwoven through the lengthwise fibers 120 to an edge of a section, such as section 48, and then extend about the edge and back through the lengthwise fibers 120 substantially without break. That is, the crosswise fibers 124 are looped about the edgemost lengthwise fibers without a break in the crosswise fibers.
- the crosswise fibers of one section may extend through the intersection with another section to form the crosswise fibers of that other section.
- FIG. 6 shows schematically the interweaving of fibers of the woven fabric connector embodiment of FIG. 3.
- This connector also includes lengthwise fibers 130 interwoven with crosswise fibers 134, 138 and 142.
- the crosswise fibers 134 are shown interwoven with the lengthwise fibers 130 to form section 72 (as also shown in FIG. 3.
- crosswise fibers 138 and 142 are interwoven with lengthwise fibers to form section 76 and 80 respectively. It is noted that the crosswise fibers in each of the sections do not extend into the other sections, other than extending to and about the fibers or fiber bundles 146 and 150 which are common to intersecting sections.
- FIG. 7 is a schematic showing of the interweaving of the fibers for the woven fabric connector embodiment of FIG. 4.
- crosswise fibers 160 are interwoven with lengthwise fibers 164 and extend from one section through the intersection 168 to form crosswise fibers of another section.
- the crosswise fibers extend from one section through the intersection 168 to a next section, and then from that section through the intersection 168 to the third section of fabric.
- FIG. 8 shows a fragmented section of fabric which includes lengthwise fibers 180 interwoven with a continuous crosswise fiber 184.
- the crosswise fiber 184 is interwoven in one direction through the lengthwise fibers 180 and then about the edgemost lengthwise fiber and back in the other direction through the lengthwise fibers, etc. This continuous looping or weaving of the crosswise fiber forms advancing columns of weft in the fabric as generally indicated in FIG. 8.
- the fabric connectors of the present invention are advantageously woven of fiber bundles of graphite, fiberglass, Kevlar, or similar high strength material.
- all such embodiments provide a three-dimensional woven fabric connector which provides a type of three-dimensional structural support. All of the embodiments include sections which are interwoven together and intersect at a common locus or loci of points. Each of these embodiments provides strength and efficient load transfer in three dimensions.
- the connectors in addition to providing strong reliable connectors, are very lightweight.
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- Engineering & Computer Science (AREA)
- Textile Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Woven Fabrics (AREA)
- Paper (AREA)
- Ink Jet (AREA)
- Materials For Medical Uses (AREA)
- Toys (AREA)
Abstract
Description
- This invention relates to a fabric joint for providing three-dimensional structural support, to a three-dimensional woven connector formed by said joint and to the application of said joint for joining structural aircraft components.
- A type of a fabric joint connector is known from applications in the aircraft industry to join structural components such as spars or ribs to wing skin coverings. Said L-shaped fabric joint connectors are bonded by adhesive to both structural components. Although creating a light-weighted joint, typical strength and efficient load transfer in only a limited number of directions is achieved, while presenting weaknesses in other directions, which, e.g. lead to peeling problems.
- A joint known from US-A 4 395 450 contains a resin impregnated woven fabric connector with intersecting fabric panels which are interwoven with an intermediate laterally extending panel. The connector is used for joints of aircraft structural members. The fiber orientation is predominately transverse.
- Woven fabric material for high load applications is known from US-A 3 991 249 and US-A 3 090 406 in which intersecting fabric sections use at least one common weft thread. The line of intersection between the sections of the fabric material extends perpendicular to the weaving or warp direction.
- DE-C 357 353 and US-A 3 538 957 disclose three-dimensional fabric having lines of intersection between connected sections of the fabric, said lines of intersection extending in weaving or warp direction.
- It is a task of the invention to create a fabric joint for providing three-dimensional structural support for at least two adjoining structural members which is useable as a connector providing strenght and efficient load transfer in a multiplicity of directions and which uniformly distributes loads and stresses between joined structural components.
- This is achieved with a fabric joint according to claim 1, which can be used as a three-dimensional woven connector according to
claim 12 for forming a joint according to claim 19. - With this configuration, strength and efficiency and uniform load transfer is provided in lengthwise and crosswise directions of the fiber bundles or fiber strands. Preferred embodiments are disclosed in the depending claims.
- Embodiments of the invention are described in accordance with the drawings, in which:
- FIG. 1 shows a fragmented, cross-sectional view of a prior art arrangement for connecting a structural support to a structural covering;
- FIG. 2 is a fragmented, cross-sectional view of a three-dimensional woven connector, in the form of an H, made in accordance with the principles of the present invention;
- FIG. 3 is a cross-sectional view of another embodiment of a three-dimensional woven connector, in the form of a T with two legs;
- FIG. 4 is a cross-section of another embodiment of a three-dimensional woven connector in the form of a Y;
- FIG. 5 is a perspective view of a schematic showing of the crosswise fibers interwoven with the lengthwise fibers of the connector embodiment of FIG. 2;
- FIG. 6 is a perspective view of a schematic showing of the crosswise fibers interwoven with the lengthwise fibers of the connector embodiment of FIG. 3;
- FIG. 7 is a perspective view of a schematic showing of the crosswise fibers interwoven with the lengthwise fibers of the connector embodiment of FIG. 4; and
- FIG. 8 is a fragmented view showing the manner in which crosswise fibers may be interwoven with lengthwise fibers in the woven connector of the present invention.
- FIG. 1 shows a prior art arrangement for connecting a spar or rib 4 (such as might be used in construction of an airplane wing) to another structural component 8 (such as the skin or covering of an aircraft wing). Placed at the joint of the spar 4 and structural component 8 to hold the two together are a pair of
fabric connectors 12 and 16 (shown in cross section in FIG. 1). A portion of eachfabric connector arrows 20 relative to one another. However, the strength of the connector is very weak when the two components are moved in the direction indicated byarrows - The three-dimensional woven fabric connector of the present invention avoids the problems outlined in connection with the FIG. 1 arrangement, and one embodiment of the connector is shown in fragmented, cross-sectional view in FIG. 2. This embodiment is shown connecting a
spar 34 to a skin covering 38, such as used in the construction of aircraft. It is noted that both thespar 34 and skin covering 38 are shown as being made of a sandwich wall construction. It should be understood that the woven fabric connectors of the present invention may be used to connect together a variety of structural components in addition to those shown in the drawings. - The connector embodiment of FIG. 2 includes a first section of
fabric 40 composed of fibers interwoven together in a cross-hatched pattern as will be described in detail later. Also included are second and third sections offabric fabric first section 40 alongrespective intersections section 44 intersectssection 40 and the locus of points at whichsection 48 intersectssection 40 are spaced apart and generally parallel in the plane ofsection 40. As will be explained further later on, at least one fiber or fiber bundle of the section offabric 40 is common with the section offabric 44, and at least one other fiber or fiber bundle ofsection 40 is common withsection 48. - As seen in FIG. 2, portions of both
sections section 40 and portions also extend downwardly therefrom. Likewise, a portion ofsection 40 extends outwardly in one direction fromsection 44, and another portion ofsection 40 extends outwardly in the opposite direction fromsection 48, with an intermediate portion ofsection 40 extending betweensections sections section 40 at right angles, but other angles of intersection could also be used as needed. Additionally, the fabric sections are bendable and thus may be made to conform to variety of shapes to which they might be bonded. - The
spar 34 andskin cover 38 are connected together by placingsection 44 flat against the underside of the skin covering 38 and bonding it thereto. The two upper portions ofsections spar 34 is placed between the two lowermost portions ofsections sections spar 34 may have relative to the skin covering 38. - FIG. 3 is a cross-sectional view of another embodiment of the woven fabric connector of the present invention. This embodiment also is shown coupling together a
spar 64 to a skin covering 68. The connector of FIG. 3 includes a first section ofwoven fabric 72, and second and third sections ofwoven fabric section 72 to extend downwardly therefrom as shown. The sections offabric 76 and 78 intersect the section offabric 72 along generally parallel loci of points at which intersections a fiber or bundle of fibers is common with thesection 72 andrespective sections - The connector of FIG. 3 is utilized by placing
section 72 flat against the bottom surface of the skin covering 68 and bonding it thereto. Thespar 64 is positioned betweensections section 72. - FIG. 4 shows a cross-sectional view of still another embodiment of the woven fabric connector of the present invention. Specifically, two
connectors 84 and 88 are shown interconnecting, at a right angle, the edges of two skin covers 92 and 96. Each of the connectors, such asconnector 84, includes threesections 100, 104 and 108, all of which extend generally radially outwardly from an intersection 112 of the three sections. The three sections are composed of fibers interwoven together, with at least one fiber or bundle of fibers being common to the three sections. - The connector 88 is similar to the
connector 84 except two of the sections are bent to overlie the outside corner of the joint of the twoskin coverings 92 and 96, as shown. Two of the sections ofconnectors 84 and 88 extend into the joint between theskin coverings 92 and 96 generally in planes parallel to one another. The different sections of the twoconnectors 84 and 88 are bonded to the surfaces of the skin coverings with which they are placed in contact. - FIG. 5 shows a schematic representation of the weaving of the connector embodiment of FIG. 2. The connector incudes lengthwise fibers or fiber bundles 120 which serve as the warp of the woven fabric. Interlaced through the lengthwise fibers 120 or warp are crosswise fibers or
fiber bundles 124 which serve as the weft of the fabric. Thecrosswise fibers 124 ofsection 48 are interwoven about a lengthwise fiber or bundle offibers 56 which is common and serves as an intersection withsection 40. Similarly, thecrosswise fibers 124 of thesection 44 are interwoven with a lengthwise fiber or bundle offibers 52 which is also common with thesection 40. The common fiber orfiber bundle 52 is spaced from and generally parallel with the fiber orfiber bundle 56, as indicated in FIG. 5. - The
crosswise fibers 124 are interwoven through the lengthwise fibers 120 to an edge of a section, such assection 48, and then extend about the edge and back through the lengthwise fibers 120 substantially without break. That is, thecrosswise fibers 124 are looped about the edgemost lengthwise fibers without a break in the crosswise fibers. Although not indicated in the FIG. 5 embodiment, the crosswise fibers of one section may extend through the intersection with another section to form the crosswise fibers of that other section. - FIG. 6 shows schematically the interweaving of fibers of the woven fabric connector embodiment of FIG. 3. This connector also includes
lengthwise fibers 130 interwoven withcrosswise fibers lengthwise fibers 130 to form section 72 (as also shown in FIG. 3. Similarly, crosswisefibers section fiber bundles - FIG. 7 is a schematic showing of the interweaving of the fibers for the woven fabric connector embodiment of FIG. 4. In this embodiment, crosswise fibers 160 are interwoven with lengthwise fibers 164 and extend from one section through the
intersection 168 to form crosswise fibers of another section. In FIG. 7 the crosswise fibers extend from one section through theintersection 168 to a next section, and then from that section through theintersection 168 to the third section of fabric. - FIG. 8 shows a fragmented section of fabric which includes lengthwise
fibers 180 interwoven with a continuouscrosswise fiber 184. Thecrosswise fiber 184 is interwoven in one direction through thelengthwise fibers 180 and then about the edgemost lengthwise fiber and back in the other direction through the lengthwise fibers, etc. This continuous looping or weaving of the crosswise fiber forms advancing columns of weft in the fabric as generally indicated in FIG. 8. - The fabric connectors of the present invention are advantageously woven of fiber bundles of graphite, fiberglass, Kevlar, or similar high strength material.
- Although different specific embodiments of the invention have been described, all such embodiments provide a three-dimensional woven fabric connector which provides a type of three-dimensional structural support. All of the embodiments include sections which are interwoven together and intersect at a common locus or loci of points. Each of these embodiments provides strength and efficient load transfer in three dimensions. The connectors, in addition to providing strong reliable connectors, are very lightweight.
- It is to be understood that the above-described arrangements are only illustrative of the application of the principles of the present invention. Numerous modifications and alternative arrangements may be devised by those skilled in the art without departing from the scope of the present invention and the appended claims are intended to cover such modifications and arrangements.
Claims (20)
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AT86106650T ATE57398T1 (en) | 1986-05-15 | 1986-05-15 | CONNECTION WITH THREE-DIMENSIONAL FABRIC. |
DE8686106650T DE3674922D1 (en) | 1986-05-15 | 1986-05-15 | CONNECTION TO THREE-DIMENSIONAL TISSUE. |
EP86106650A EP0245533B1 (en) | 1986-05-15 | 1986-05-15 | Three dimensional woven fabric connector |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP86106650A EP0245533B1 (en) | 1986-05-15 | 1986-05-15 | Three dimensional woven fabric connector |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0245533A1 EP0245533A1 (en) | 1987-11-19 |
EP0245533B1 true EP0245533B1 (en) | 1990-10-10 |
Family
ID=8195126
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP86106650A Expired EP0245533B1 (en) | 1986-05-15 | 1986-05-15 | Three dimensional woven fabric connector |
Country Status (3)
Country | Link |
---|---|
EP (1) | EP0245533B1 (en) |
AT (1) | ATE57398T1 (en) |
DE (1) | DE3674922D1 (en) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4671470A (en) * | 1985-07-15 | 1987-06-09 | Beech Aircraft Corporation | Method for fastening aircraft frame elements to sandwich skin panels covering same using woven fiber connectors |
JPH0791725B2 (en) * | 1988-02-29 | 1995-10-04 | 三菱重工業株式会社 | Three-dimensional fabric with irregular cross section |
US5343897A (en) * | 1988-02-29 | 1994-09-06 | Mitsubishi Jukogyo Kabushiki Kaisha | Profiled cross-section three dimensional woven fabric |
US20030116267A1 (en) * | 2001-12-21 | 2003-06-26 | Sheahen Patrick D. | Low-cost method of assembling structures with 3-D woven connectors |
US8082667B2 (en) | 2007-05-31 | 2011-12-27 | The Boeing Company | Apparatus and methods for securing a first structural member and a second structural member to one another |
US10513325B2 (en) * | 2016-02-08 | 2019-12-24 | Bell Helicopter Textron Inc. | Joint member for a composite wing structure |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE357353C (en) * | 1921-07-24 | 1922-08-23 | Hermann Borgmann | Process for the production of folded fabrics with folds running in the direction of the warp |
US3090406A (en) * | 1961-02-23 | 1963-05-21 | Raymond Dev Ind Inc | Woven panel and method of making same |
GB1099626A (en) * | 1963-12-12 | 1968-01-17 | French & Sons Thomas | Improvements in or relating to woven curtain heading tape |
US3538957A (en) * | 1968-08-19 | 1970-11-10 | Hitco | Three-dimensional woven fabric |
US4395450A (en) * | 1981-09-30 | 1983-07-26 | The Boeing Company | Composite structural skin spar joint and method of making |
-
1986
- 1986-05-15 EP EP86106650A patent/EP0245533B1/en not_active Expired
- 1986-05-15 AT AT86106650T patent/ATE57398T1/en not_active IP Right Cessation
- 1986-05-15 DE DE8686106650T patent/DE3674922D1/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
EP0245533A1 (en) | 1987-11-19 |
DE3674922D1 (en) | 1990-11-15 |
ATE57398T1 (en) | 1990-10-15 |
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